IT1117626B - Rotore articolato per elicotteri - Google Patents
Rotore articolato per elicotteriInfo
- Publication number
- IT1117626B IT1117626B IT67223/79A IT6722379A IT1117626B IT 1117626 B IT1117626 B IT 1117626B IT 67223/79 A IT67223/79 A IT 67223/79A IT 6722379 A IT6722379 A IT 6722379A IT 1117626 B IT1117626 B IT 1117626B
- Authority
- IT
- Italy
- Prior art keywords
- helicopters
- articulated rotor
- articulated
- rotor
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/322—Blade travel limiting devices, e.g. droop stops
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/35—Rotors having elastomeric joints
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pivots And Pivotal Connections (AREA)
- Braking Arrangements (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67223/79A IT1117626B (it) | 1979-02-02 | 1979-02-02 | Rotore articolato per elicotteri |
DE3001207A DE3001207C2 (de) | 1979-02-02 | 1980-01-15 | Gelenk-Rotor für Hubschrauber |
US06/113,726 US4342540A (en) | 1979-02-02 | 1980-01-21 | Articulated rotor for helicopters |
GB8002622A GB2041310B (en) | 1979-02-02 | 1980-01-25 | Blade-to-hub connections for helicopter rotors |
JP888280A JPS55106897A (en) | 1979-02-02 | 1980-01-30 | Articulated rotor for helicopter |
FR8002159A FR2447856A1 (fr) | 1979-02-02 | 1980-01-31 | Rotor articule pour helicoptere |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67223/79A IT1117626B (it) | 1979-02-02 | 1979-02-02 | Rotore articolato per elicotteri |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7967223A0 IT7967223A0 (it) | 1979-02-02 |
IT1117626B true IT1117626B (it) | 1986-02-17 |
Family
ID=11300620
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT67223/79A IT1117626B (it) | 1979-02-02 | 1979-02-02 | Rotore articolato per elicotteri |
Country Status (6)
Country | Link |
---|---|
US (1) | US4342540A (ja) |
JP (1) | JPS55106897A (ja) |
DE (1) | DE3001207C2 (ja) |
FR (1) | FR2447856A1 (ja) |
GB (1) | GB2041310B (ja) |
IT (1) | IT1117626B (ja) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1117626B (it) * | 1979-02-02 | 1986-02-17 | Aereonautiche Giovanni Augusta | Rotore articolato per elicotteri |
IT1129070B (it) * | 1980-04-03 | 1986-06-04 | Agusta Aeronaut Costr | Rotore a giunti elastomerici per elicotteri |
IT1143358B (it) * | 1981-02-05 | 1986-10-22 | Agusta Aeronaut Costr | Mozzo composito di un rotore di elicottero |
FR2516891A1 (fr) * | 1981-11-25 | 1983-05-27 | Aerospatiale | Rotor pour giravions, a articulations integrees dans le pied de pale |
US4419051A (en) * | 1982-02-16 | 1983-12-06 | The Boeing Company | Twin tension/torsion beam rotor system |
IT1155132B (it) * | 1982-03-11 | 1987-01-21 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1155131B (it) * | 1982-03-11 | 1987-01-21 | Agusta Aeronaut Costr | Mozzo di rotore di elicotteri |
FR2529860B1 (fr) * | 1982-07-08 | 1987-01-02 | Aerospatiale | Plateau de moyeu, procede de fabrication et moyeu de rotor de giravion equipe de tels plateaux |
US4543040A (en) * | 1982-09-30 | 1985-09-24 | The Boeing Company | Helicopter rotor system |
DE3241754C2 (de) * | 1982-11-11 | 1986-02-06 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor, insbesondere eines Drehflügelflugzeuges |
IT1157122B (it) * | 1982-12-06 | 1987-02-11 | Agusta Aeronaut Costr | Rotore per elicottero |
IT1159375B (it) * | 1983-03-15 | 1987-02-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
US4568244A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Fiber reinforced/epoxy matrix composite helicopter rotor main hub plate |
US4568245A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Composite helicopter rotor hub |
IT1205405B (it) * | 1983-05-05 | 1989-03-15 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1182448B (it) * | 1985-02-19 | 1987-10-05 | Agusta Aeronaut Costr | Mozzo metallico per un rotore di elicottero |
IT1182447B (it) * | 1985-02-19 | 1987-10-05 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1196801B (it) * | 1986-11-25 | 1988-11-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1196800B (it) * | 1986-11-25 | 1988-11-25 | Agusta Aeronaut Costr | Rotore anticoppia per elicotteri |
DE3801010A1 (de) * | 1988-01-15 | 1989-08-03 | Messerschmitt Boelkow Blohm | Rotor, insbesondere fuer ein drehfluegelflugzeug |
FR2630703B1 (fr) * | 1988-04-29 | 1990-08-24 | Aerospatiale | Tete de rotor de giravion a tirants interpales de rappel elastique avec amortissement incorpore |
FR2648106B1 (fr) * | 1989-06-08 | 1991-09-27 | Aerospatiale | Dispositif de butees escamotables pour pales de rotors de giravions, et tete de rotor le comportant |
FR2728540A1 (fr) * | 1994-12-22 | 1996-06-28 | Eurocopter France | Rotor sans articulation a anneaux intermediaires de commande de pas |
IT1282114B1 (it) * | 1995-06-09 | 1998-03-12 | Augusta S P A | Rotore per elicotteri. |
FR2764577B1 (fr) * | 1997-06-13 | 1999-08-20 | Eurocopter France | Rotor de giravion a butees de battement fixes sur pales et moyeu, et a loi pas-battement determinee |
FR2764578B1 (fr) | 1997-06-13 | 1999-09-10 | Eurocopter France | Rotor de giravion a moyeu bi-plateau et commande de pas partiellement externe |
ITTO20020509A1 (it) * | 2002-06-14 | 2003-12-15 | Agusta Spa | Mozzo per un rotore di un elicottero e rotore provvisto di tale mozzo |
WO2010068194A1 (en) | 2008-12-09 | 2010-06-17 | Sikorsky Aircraft Corporation | Lead stop for rotor system with fluid-elastomeric lead/lag damper |
US8695918B2 (en) | 2012-01-10 | 2014-04-15 | Bell Helicopter Textron Inc. | Bearing restraint for rotor systems |
US9156544B2 (en) | 2012-02-21 | 2015-10-13 | Textron Innovations Inc. | Hub assembly with centrifugal and radial bearings |
US9308992B2 (en) | 2012-02-28 | 2016-04-12 | Sikorsky Aircraft Corporation | Helicopter blade retention composite yoke |
US9656747B2 (en) * | 2013-03-14 | 2017-05-23 | Bell Helicopter Textron Inc. | Soft in-plane and stiff out-of-plane rotor system |
FR3017108A1 (fr) | 2014-01-31 | 2015-08-07 | Airbus Helicopters | Rotor pour giravion comportant un mecanisme de butee en battement, et giravion |
US9764831B2 (en) * | 2014-03-10 | 2017-09-19 | Bell Helicopter Textron Inc. | Articulated main rotor hub with inwardly CF bearing and 3% flapping hinge offset |
FR3029892B1 (fr) | 2014-12-11 | 2017-01-06 | Airbus Helicopters | Dispositif de liaison par une rotule lamifiee entre une pale d'un rotor de giravion et un amortisseur de trainee de ladite pale |
FR3034077B1 (fr) | 2015-03-27 | 2018-05-04 | Airbus Helicopters | Mecanisme de butee en battement d'un ensemble sustentateur, rotor pour giravion comportant ce mecanisme de butee, et giravion |
FR3053312B1 (fr) * | 2016-06-29 | 2019-07-19 | Airbus Helicopters | Rotor et aeronef pourvu d'un tel rotor |
US10773798B2 (en) * | 2017-09-29 | 2020-09-15 | Bell Textron Inc. | Rotor hub with blade-to-blade dampers attached to the pitch change axis |
US10597150B2 (en) * | 2018-04-24 | 2020-03-24 | Textron Innovations Inc. | Articulated rotor systems with blade-to-blade damping |
WO2019217532A1 (en) * | 2018-05-08 | 2019-11-14 | Avx Aircraft Company | Rotor hub |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH212105A (de) * | 1938-02-12 | 1940-10-31 | Flettner Anton | Hubschrauber mit paarweise ineinander kämmenden Rotoren. |
US3147810A (en) * | 1962-09-12 | 1964-09-08 | Boeing Co | Restraining mechanism |
US3282350A (en) * | 1965-10-20 | 1966-11-01 | Boeing Co | Rotor blade mounting construction |
FR2125150B1 (ja) * | 1971-02-15 | 1973-12-07 | Aerospatiale | |
US3700352A (en) * | 1971-03-05 | 1972-10-24 | Lord Corp | Rotor system |
US3761199A (en) * | 1972-07-14 | 1973-09-25 | United Aircraft Corp | Helicopter rotor with redundant load carrying capability |
GB1432117A (en) * | 1973-05-10 | 1976-04-14 | Aerospatiale | Rotor for rotating wing type aircraft |
FR2228663A1 (en) * | 1973-05-10 | 1974-12-06 | Aerospatiale | Rotor for rotating wing aircraft - has yoke connecting rotor arm and star shaped rotor has low weight |
FR2305343A2 (fr) * | 1975-03-26 | 1976-10-22 | Aerospatiale | Rotor pour giravions |
US4012169A (en) * | 1973-05-10 | 1977-03-15 | Societe Nationale Industrielle Aerospatiale | Rotor for rotating wing type aircraft |
JPS5852880B2 (ja) * | 1973-09-14 | 1983-11-25 | ユナイテッド・テクノロジ−ズ・コ−ポレイション | 関節式ヘリコプタロ−タ |
US3932059A (en) * | 1975-01-10 | 1976-01-13 | United Technologies Corporation | Droop stops for helicopter rotor having elastomeric bearings |
JPS5264797A (en) * | 1975-11-26 | 1977-05-28 | Kawasaki Heavy Ind Ltd | Rotor head of rotary cascade aircraft |
US4178130A (en) * | 1976-04-06 | 1979-12-11 | United Technologies Corporation | Helicopter rotor having lead-lag damper operable with pitch and flap decoupling |
US4105365A (en) * | 1976-10-04 | 1978-08-08 | United Technologies Corporation | Helicopter rotor lead-lag damper |
DE2648343C3 (de) * | 1976-10-26 | 1981-06-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag- und schwenkgelenkloser Rotor für Drehflügelflugzeuge |
US4135856A (en) * | 1977-02-03 | 1979-01-23 | Lord Corporation | Rotor blade retention system |
GB2025338B (en) * | 1978-06-02 | 1982-08-04 | Aerospatiale | Helicopterrotor |
FR2427251A1 (fr) * | 1978-06-02 | 1979-12-28 | Aerospatiale | Rotor pour giravion |
US4203708A (en) * | 1978-06-26 | 1980-05-20 | United Technologies Corporation | Elastomeric rotor load reaction system |
US4235570A (en) * | 1978-06-26 | 1980-11-25 | United Technologies Corporation | Elastomeric helicopter rotor load reaction system |
FR2434079A1 (fr) * | 1978-08-23 | 1980-03-21 | Aerospatiale | Dispositif pour limiter les battements des pales d'un rotor principal de giravion |
US4257739A (en) * | 1978-09-11 | 1981-03-24 | Textron, Inc. | Soft inplane helicopter rotor |
IT1117626B (it) * | 1979-02-02 | 1986-02-17 | Aereonautiche Giovanni Augusta | Rotore articolato per elicotteri |
-
1979
- 1979-02-02 IT IT67223/79A patent/IT1117626B/it active
-
1980
- 1980-01-15 DE DE3001207A patent/DE3001207C2/de not_active Expired - Lifetime
- 1980-01-21 US US06/113,726 patent/US4342540A/en not_active Expired - Lifetime
- 1980-01-25 GB GB8002622A patent/GB2041310B/en not_active Expired
- 1980-01-30 JP JP888280A patent/JPS55106897A/ja active Granted
- 1980-01-31 FR FR8002159A patent/FR2447856A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
US4342540A (en) | 1982-08-03 |
JPS55106897A (en) | 1980-08-16 |
FR2447856A1 (fr) | 1980-08-29 |
GB2041310A (en) | 1980-09-10 |
GB2041310B (en) | 1983-05-25 |
FR2447856B1 (ja) | 1984-04-13 |
JPH0129759B2 (ja) | 1989-06-13 |
IT7967223A0 (it) | 1979-02-02 |
DE3001207C2 (de) | 1994-03-31 |
DE3001207A1 (de) | 1980-08-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19970227 |